STC SA4836NM

Supplemental type certificate · ACSS (Aviation Communication and Surveillance Syst

Holder
ACSS (Aviation Communication and Surveillance Syst · United States
Status
Current · Reissued
Status date
February 28, 2002
Applied
July 24, 1989
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA22WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of provisions for wiring and hardware for Honeywell Traffic Alert and Collision Avoidance System (TCAS II).

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

~l1itdl j&tates Ql}f,America JElepnrtnt£ut of 'illrnusportntiou - JIfebernl ~&intiou J\bmiuistrntiou, ACSS (Aviation Communication & Surveillance Systems, LLC) 19810 North ih Avenue Phoenix, AZ 85027 c('•...,,(,;4~~a// ~ r:A:r£/,:?~Vb ~ 1?/tt' rk'Jrp....I,ftP ~ ftllbmr/tp /'rorbu;/ rrf//£ ~ t'foMH/£rfJ/l-). a/14 CO/I.£k"/l!rm~Jaer~pe a-J ,y-t('-erj4"ed'&rl"o/I, nt('('/,J ~ al!;l!uopd/,~,J-J rr,?l!u/-('//t('/I/,J 0/ ,cjpar/ FAR 25* 0/ ae .%rknNf ..ArHff£rO/I_ .5Y6epa&/I!O/M. *(For Certification basis see Type Certificate Data Sheet A22WE.)

..46orke.' DC-1O-1O/-lOF/-15/-30/-30F/-40/-40F Series f!Zc~CP~-t/I!O/i' o/J?;/'e ~";'~b ?5}{;utpr'.. Installation of Honeywell Traffic Alert and Collision Avoidance System (TCAS II) in accordance with FAA approved Honeywell Master Data List Number ML4070452, Revision "C", dated August 31, 1990, or later FAA approved Revision. Honeywell, Inc., Flight Manual Supplement Document No. 5140-0882, FAA approved on September 5, 1990, or later approved revision is required as part of this installation.

For appropriate FAA approved Airplane Flight Manual Supplement refer to associated section of the Honeywell Master Data List.

5E"nM"/a/I!O/',J ru,d~/,~uo/i-J ..This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. See also specific appendices for additional limitations. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission .

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January 22, 1990 .r!!&//e,rn;;";."er/.' February 28, 2002 (Signature) , Tech. and Admin. Support Staff eles Aircraft Certification Office (Title) ffny aCtuation of this ctrtificate is punisfia6fe 6y a Jim of not e:{cwfing $1,000, or imprisonmlnt not e;lJ:w£ing 3 years, or 60th.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 7

MakeModelData sheet
McDonnell Douglas CorporationDC-10-10A22WE
McDonnell Douglas CorporationDC-10-10FA22WE
McDonnell Douglas CorporationDC-10-15A22WE
McDonnell Douglas CorporationDC-10-30A22WE
McDonnell Douglas CorporationDC-10-30FA22WE
McDonnell Douglas CorporationDC-10-40A22WE
McDonnell Douglas CorporationDC-10-40FA22WE